WO2015161048A1 - Ensemble de fixation pour couverture isolante - Google Patents
Ensemble de fixation pour couverture isolante Download PDFInfo
- Publication number
- WO2015161048A1 WO2015161048A1 PCT/US2015/026127 US2015026127W WO2015161048A1 WO 2015161048 A1 WO2015161048 A1 WO 2015161048A1 US 2015026127 W US2015026127 W US 2015026127W WO 2015161048 A1 WO2015161048 A1 WO 2015161048A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fastener
- cap member
- cap
- substrate
- insulation blanket
- Prior art date
Links
- 238000009413 insulation Methods 0.000 title claims abstract description 52
- 239000000758 substrate Substances 0.000 claims abstract description 42
- 239000002184 metal Substances 0.000 claims description 10
- 229910052751 metal Inorganic materials 0.000 claims description 10
- 239000004033 plastic Substances 0.000 claims description 9
- 239000004642 Polyimide Substances 0.000 claims description 5
- 229920001721 polyimide Polymers 0.000 claims description 5
- 229910001220 stainless steel Inorganic materials 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 238000010276 construction Methods 0.000 abstract description 5
- 239000000853 adhesive Substances 0.000 description 7
- 230000001070 adhesive effect Effects 0.000 description 7
- 239000000463 material Substances 0.000 description 7
- 239000002131 composite material Substances 0.000 description 6
- 239000007767 bonding agent Substances 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000012774 insulation material Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004382 potting Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 230000003685 thermal hair damage Effects 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/14—Cap nuts; Nut caps or bolt caps
- F16B37/145—Sleeve nuts, e.g. combined with bolts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/40—Sound or heat insulation, e.g. using insulation blankets
- B64C1/403—Arrangement of fasteners specially adapted therefor, e.g. of clips
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/04—Devices for fastening nuts to surfaces, e.g. sheets, plates
- F16B37/048—Non-releasable devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B37/00—Nuts or like thread-engaging members
- F16B37/14—Cap nuts; Nut caps or bolt caps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/06—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips
- F16B5/0692—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of clamps or clips joining flexible sheets to other sheets or plates or to strips or bars
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/74—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls
- E04B1/76—Heat, sound or noise insulation, absorption, or reflection; Other building methods affording favourable thermal or acoustical conditions, e.g. accumulating of heat within walls specifically with respect to heat only
- E04B1/762—Exterior insulation of exterior walls
- E04B1/7629—Details of the mechanical connection of the insulation to the wall
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Definitions
- the present invention relates to mounts and fasteners. More specifically, the present invention relates to fasteners for affixing thermal insulation blankets to a substrate, such as the engine nacelles of an aircraft.
- an “attachment member” such as a fastener or the like
- a substrate For example, it is known to mount threaded fasteners or the like onto a substrate so as to be able to attach additional components to the substrate's surface.
- Adhesive bonded attachments are well known for connecting a component to a threaded stud or bolt so as to mount components to a substrate.
- These adhesive attachment members typically include a base providing a bonding surface which is adapted to receive a curable bonding agent. The base is then pressed against the substrate surface so as to allow the bonding agent to cure.
- Attachment members including a base and male or female threaded fastener have been used to support and affix thermal insulation blankets to a substrate wherein the insulation blanket is provided to act as a heat-shield to protect surrounding structures and components.
- thermal insulation blankets have been mounted on the inboard side of aircraft engine nacelles.
- a thermal insulation blanket is made of a refractory cloth material which includes multiple grommets forming mounting holes for affixing the blanket to the substrate.
- a plurality of adhesive bonded attachment members are affixed to the nacelle substrate at various positions with the attachment members' male or female threaded elements projecting through the insulation blanket's mounting holes. Separate cooperative threaded elements, such as nuts or bolts, are then secured to the attachment member's threaded elements for retaining the insulation blanket in place.
- U.S. Patent No. 7,584,582 which is incorporated by reference herein, discloses an adhesive bonded attachment assembly for use in affixing insulation blankets to a substrate.
- the attachment assembly includes an attachment member including a base for adhesively affixing to a substrate as well as a threaded element for projecting through an insulation blanket's mounting hole.
- the assembly includes a cap having a radially enlarged cap member and a second threaded element for affixing to the attachment member.
- the cap member has a size so as to overlie and engage the insulation blanket so as to keep it in place.
- the cap member has an inboard piece and an outboard piece forming an internal chamber.
- the cap's inboard piece and outboard piece are typically made of metal and an insulation material is positioned within the cap's central chamber.
- the fastener assembly described in U.S. Patent No. 7,584,582 suffers from several drawbacks.
- the fastener assembly is primarily made of metal, the assembly is undesirably heavy.
- the cap fastener is made of multiple components which must be assembled together thereby introducing undesirable complexity. All-metal fasteners provide extremely high strength to a fastener element.
- adhesives and potting materials typically do not bond well to an all-metal material, such as titanium, as well as to a composite or plastic material.
- metal fasteners are typically heavy and expensive.
- plastic fasteners provide low weight, but lesser strength values than all-metal fasteners.
- an improved fastener assembly for affixing thermal insulation blankets to a substrate.
- the assembled components are described herein as including the substrate and thermal insulation blanket.
- substrate is intended to be interpreted broadly as to include any surface or fixtures upon which an insulation blanket is to be mounted.
- insulation blanket is to be interpreted broadly to include any material, flexible or otherwise, providing thermal protection, either from conduction, convection or radiation.
- the fastener assembly further includes an attachment member attached to the substrate.
- the attachment member may be constructed in various manners as can be determined by those skilled in the art to provide a structure upon which a second part of a fastener can be fastened.
- the attachment member includes an enlarged base providing a mounting surface for adhesive affixation to the substrate.
- the attachment member include a first fastener element, such as in the form of a male or female threaded element.
- this first fastener element be male or female threaded, other known fastener constructions can be utilized.
- the fastener assembly of the present invention further includes a cap fastener.
- the cap fastener includes a radially enlarged cap member having a radial size and shape greater than an insulation blanket mounting hole.
- the cap member includes an exterior side and an interior side.
- the cap fastener further includes a second fastener element extending from the cap member's interior side.
- the second fastener element may be constructed in any manner so as to affix to the attachment member's first fastener element.
- this second fastener element be a male or female extension of a size so as to project at least partially through the insulation blanket's mounting hole to affix to a cooperatively constructed first fastener element adhered to the substrate.
- first and second fastener elements may include hook and pile, snaps, press-fit arrangements, etc.
- the cap fastener include a construction to allow it to be manually rotated, and thereby affixed, relative to the attachment member.
- various known constructions for rotating the cap fastener may be selected by those skilled in the art including slots for a standard or Phillips screwdriver.
- a preferred construction includes a hexagonal projection formed upon the cap member's exterior side for mating to a socket tool.
- this hexagonal projection has a diameter smaller than the diameter of the enlarged cap member.
- the cap member's interior surface includes a circular recess surrounding the second fastener element.
- the circular recess forms a circular insulating cavity between the cap member and insulation blanket which provides additional insulation and reduced heat transfer through the fastener assembly.
- the cap member's interior surface has a substantially concave shape so as to form the circular recess surrounding the second fastener element.
- the various components of the fastener assembly may be made of various materials.
- the attachment member include a base made of composite or plastic material such as woven polyimide.
- the cap fastener's cap member be made of composite or plastic material such as woven polyimide.
- these threaded components be made of metal, such as a 300 series stainless steel.
- FIG. 1 is an exploded top perspective view of the fastener assembly for insulation blanket of the present invention
- FIG. 2 is a bottom perspective view of the fastener assembly for insulation blanket of the present invention
- FIG. 3 is a top partial cut-away perspective view of the cap fastener of the present invention.
- FIG. 4 is a side cut-away view of the fastener assembly for insulation blanket of the present invention.
- FIG. 5 is a top perspective exploded view of the fastener assembly of the present invention including insulation blanket and substrate;
- FIG. 6 is a side cut-away view of the fastener assembly for insulation blanket of the present invention including insulation blanket and substrate.
- the fastener assembly 1 of the present invention is for use in supporting and affixing an insulation blanket 5 to a substrate 3, such as an aircraft engine nacelle.
- the substrate 3 is a wall panel or the like that separates an environment having a relatively high temperature from another environment having cooler temperatures. It is anticipated that the substrate is typically formed from light weight metals or composite materials which may form the nacelle for an aircraft engine.
- the insulation blanket 5 is mounted to the substrate 3 to insulate and thereby safeguard adjacent structures and components from undesirable thermal damage.
- the insulation blanket 5 may include exterior refractory materials as well as multiple internal insulating layers.
- the insulation blanket 5 includes one or more mounting holes 11 which preferably are lined with grommets 9. As illustrated in FIG. 5, preferably each grommet 9 has a round short rim.
- the fastener assembly 1 includes two primary components including an attachment member 21 affixed to the substrate 3 and a cap fastener 31 for holding the insulation blanket 5 in place.
- the attachment member 21 includes a flat base 23 and a first fastener member 25, which as illustrated in the figures, is preferably a male threaded stud.
- the attachment member may include an alignment tab 27.
- the alignment tab 27 projects downwardly from the base 23 and is provided only where the substrate 3 includes a hole or notch for receiving and positioning the attachment member 21.
- the base 23 is made of a plastic, such as a woven polyimide and has a flat bottom surface for affixing to the substrate 5 using an adhesive 13.
- the fastener assembly's cap fastener 31 includes a cap member 33 which is preferably round and has an exterior side 35 and an interior side 37. As illustrated in FIGS. 5 and 6, the cap member 33 is radially enlarged so as to have a size and shape greater than the insulation blanket's mounting hole 11.
- the cap fastener 31 further includes a second fastener member 45 capable of fastening to the attachment member's first fastener member 25. As illustrated, the cap fastener's second fastener member is preferably a female threaded extension 45 sized to affix to the attachment member's male threaded stud 25.
- the cap member's interior 37 includes a circular recess 39 which is concentrically formed around the female threaded extension 45. As best illustrated in FIG. 4, it is preferred that the cap member's interior side 37 have a concave shape with the female threaded extension projecting concentrically from its middle so as to form the circular recess 39. As best illustrated in FIGS. 4 and 6, the cap member's circular recess 39 forms an insulating cavity 15. More specifically, the cap member's circular recess 39 allows the periphery of the cap member to engage an insulation blanket 5 so as to maintain the insulation blanket against the substrate 3. However, the remaining circular recess 39 portion of a cap member has little or no engagement with the insulation blanket 5 so as to create the insulating cavity 15 which provides reduced thermal conduction and a corresponding increase in thermal insulation.
- the cap fastener's cap member 33 be made of a composite or plastic having excellent thermal insulation properties such as a woven polyimide.
- the cap member's second fastener member preferably a female threaded extension 45
- the female threaded extension include a head, preferably having one or more radially projecting flanges 47 which are encapsulated within the cap member 33.
- the head have a diameter larger than the diameter of the blanket's hole so that in the event that the cap member's composite or plastic failed, the fastener head would retain the blanket against the substrate.
- the attachment member's male threaded stud 25 also include a radially projecting region or flanges which are encapsulated within the attachment member's base 23.
- the cap member have a shape so as to allow it to be rotated by a tool.
- any of many keyed slots or projecting shapes may be selected by those skilled in the art.
- a preferred cap member 33 has a hexagonal projection 43 sized for receipt within a 3/4 inch hexagonal socket tool commonly carried by aircraft machinist and repairmen.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Bolts, Nuts, And Washers (AREA)
Abstract
Cette invention concerne un ensemble de fixation pour fixer des couvertures isolantes sur un substrat. Ledit ensemble de fixation comprend un élément d'attache présentant une construction permettant de le fixer à un substrat ainsi qu'un premier élément de fixation se présentant de préférence sous forme de goujon fileté mâle. Ledit ensemble de fixation comprend en outre un élément de fixation en forme de capuchon. Ledit élément de fixation en forme de capuchon comprend un élément en forme de capuchon et un second élément de fixation, de préférence en forme d'extension filetée femelle pour une fixation par filetage au premier élément de fixation. Ledit élément en forme de capuchon présente un côté extérieur et un côté intérieur. Le côté extérieur de l'élément en forme de capuchon présente de préférence une forme permettant la rotation au moyen d'un outil. Par ailleurs, le côté intérieur de l'élément en forme de capuchon présente un renfoncement circulaire concentrique avec l'extension filetée femelle de l'élément de fixation en forme de capuchon. Lorsqu'il est assemblé, le renfoncement circulaire forme une cavité isolante circulaire entre l'élément en forme de capuchon et un matelas isolant.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15780579.7A EP3132149B1 (fr) | 2014-04-17 | 2015-04-16 | Ensemble de fixation pour couverture isolante |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US14/255,537 | 2014-04-17 | ||
US14/255,537 US9470257B2 (en) | 2014-04-17 | 2014-04-17 | Fastener assembly for insulation blanket |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2015161048A1 true WO2015161048A1 (fr) | 2015-10-22 |
Family
ID=54321644
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2015/026127 WO2015161048A1 (fr) | 2014-04-17 | 2015-04-16 | Ensemble de fixation pour couverture isolante |
Country Status (3)
Country | Link |
---|---|
US (2) | US9470257B2 (fr) |
EP (1) | EP3132149B1 (fr) |
WO (1) | WO2015161048A1 (fr) |
Families Citing this family (14)
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US20160307473A1 (en) * | 2015-04-17 | 2016-10-20 | Ford Global Technologies, Llc | Nameplate assembly and fastener |
US10173612B2 (en) | 2016-10-11 | 2019-01-08 | Ford Global Technologies, Llc | Wiring attachment assembly and wiring system for a motor vehicle |
FR3059062B1 (fr) * | 2016-11-22 | 2019-07-19 | Airbus Operations | Entretoise auto-perforante pour un matelas d'isolation d'aeronef, procede de pose de ladite entretoise et matelas d'isolation d'aeronef equipe de ladite entretoise |
US10814954B2 (en) * | 2017-01-17 | 2020-10-27 | The Boeing Company | Insulation system |
JP6374627B1 (ja) * | 2017-08-17 | 2018-08-15 | 東洋ゴム工業株式会社 | タイヤ加硫金型、タイヤ加硫金型を鋳造するための鋳型、およびタイヤ加硫金型の製造方法 |
FR3073599B1 (fr) * | 2017-11-16 | 2020-01-17 | Safran Nacelles | Dispositif de fixation pour panneau de protection thermique |
US11161591B2 (en) * | 2018-07-09 | 2021-11-02 | The Boeing Company | Insulation sealing system |
USD871892S1 (en) * | 2018-09-27 | 2020-01-07 | B. Erickson Manufacturing Ltd. | Rotatable e-track |
USD883071S1 (en) * | 2018-12-18 | 2020-05-05 | Railblaza Limited | Support for boating accessories |
US11028969B2 (en) * | 2019-06-03 | 2021-06-08 | The Boeing Company | Structural interface hardware for cryogenic tanks |
US11370562B2 (en) * | 2019-10-10 | 2022-06-28 | The Boeing Company | Apparatus for attaching to aircraft structural component |
GB202101873D0 (en) * | 2021-02-11 | 2021-03-31 | Lewis Stephen Desmond | Thermal protection for supersonic and space planes |
USD1017840S1 (en) * | 2021-08-25 | 2024-03-12 | Up Way Systems, Lda. | Waterproof screw cover |
US11927137B2 (en) * | 2022-03-21 | 2024-03-12 | Ge Infrastructure Technology Llc | System and method for insulating components in an exhaust gas flow from a gas turbine |
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2014
- 2014-04-17 US US14/255,537 patent/US9470257B2/en active Active
-
2015
- 2015-04-16 EP EP15780579.7A patent/EP3132149B1/fr active Active
- 2015-04-16 WO PCT/US2015/026127 patent/WO2015161048A1/fr active Application Filing
-
2016
- 2016-10-17 US US15/295,041 patent/US10288107B2/en active Active
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US7584582B1 (en) * | 2006-02-14 | 2009-09-08 | Physical Systems, Inc. | Adhesive bonded attachment assembly for an insulation blanket |
US20090090812A1 (en) * | 2006-05-17 | 2009-04-09 | Airbus Deutschland Gmbh | Insulation of an Aircraft Fuselage Structure |
US20080226413A1 (en) * | 2007-03-16 | 2008-09-18 | Robert Stephen | Inset panel fastener |
US20130161123A1 (en) * | 2011-12-21 | 2013-06-27 | Airbus Operations (Sas) | Standardised insulation device for an aircraft and processes of making and using thereof |
Also Published As
Publication number | Publication date |
---|---|
EP3132149B1 (fr) | 2019-10-30 |
EP3132149A1 (fr) | 2017-02-22 |
US20170030397A1 (en) | 2017-02-02 |
EP3132149A4 (fr) | 2017-12-20 |
US20150300396A1 (en) | 2015-10-22 |
US10288107B2 (en) | 2019-05-14 |
US9470257B2 (en) | 2016-10-18 |
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